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contributor authorF. J. G. Heyes
contributor authorH. P. Hodson
date accessioned2017-05-08T23:42:50Z
date available2017-05-08T23:42:50Z
date copyrightJuly, 1993
date issued1993
identifier issn0889-504X
identifier otherJOTUEI-28630#376_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112783
description abstractThis paper describes a simple two-dimensional model for the calculation of the leakage flow over the blade tips of axial turbines. The results obtained from calculations are compared with data obtained from experimental studies of two linear turbine cascades. One of these cascades has been investigated by the authors and previously unpublished experimental data are provided for comparison with the model. In each of the test cases examined, excellent agreement is obtained between the experimental and predicted data. Although ignored in the past, the importance of pressure gradients along the blade chord is highlighted as a major factor influencing the tip leakage flow.
publisherThe American Society of Mechanical Engineers (ASME)
titleMeasurement and Prediction of Tip Clearance Flow in Linear Turbine Cascades
typeJournal Paper
journal volume115
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2929264
journal fristpage376
journal lastpage382
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsClearances (Engineering)
keywordsTurbines
keywordsBlades
keywordsLeakage flows
keywordsPressure gradient AND Chords (Trusses)
treeJournal of Turbomachinery:;1993:;volume( 115 ):;issue: 003
contenttypeFulltext


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